| [1] Zha G C,Im H,Espinal D.Toward zero sonic boom and high efficiency supersonic flight,Part I: a novel concept of supersonic bi-directional flying wing.AIAA-2010-1013,2010.[2] Nikolic V,Jumper E J.Zero-lift wave drag calculation using supersonic area rule and its modifications.AIAA-2004-217,2004.[3] Anderson J D.Fundamentals of aerodynamics.4th ed.Boston: McGraw-Hill,2007: 691-693.[4] Kulfan B M,Bussoletti J E."Fundamental" parametric geometry representations for aircraft component shapes.AIAA-2006-6948,2006.[5] Kulfan B M.New supersonic wing far-field composite-element wave-drag optimization method,"FCE".AIAA-2008-132,2008.[6] Guan X H,Li Z K,Song B F.Exploring optimization of supersonic wing thickness distribution using FCE (far-field composite element) method.Journal of Northwestern Polytechnical University,2012,30(2): 169-174.(in Chinese) 关晓辉,李占科,宋笔锋.基于FCE方法的超声速机翼厚度分布优化.西北工业大学学报,2012,30(2): 169-174.[7] Guan X H,Song B F,Li Z K.Extended far-field composite element supersonic wing-body wave drag optimization method.Acta Aeronautica et Astronautica Sinica,2013,34(5): 1036-1045.(in Chinese) 关晓辉,宋笔锋,李占科.超声速翼身组合体激波阻力优化的EFCE算法.航空学报,2013,34(5): 1036-1045.[8] Kulfan R M.Application of hypersonic favorable aerodynamic interference concepts to supersonic aircraft.AIAA-1978-1458,1978.[9] Guan X H,Li Z K,Song B F.A study on CST aerodynamic shape parameterization method.Acta Aeronautica et Astronautica Sinica,2012,33(4): 625-633.(in Chinese) 关晓辉,李占科,宋笔锋.CST气动外形参数化方法研究.航空学报,2012,33(4): 625-633.[10] Kulfan B M.A universal parametric geometry representation method—"CST".AIAA-2007-62,2007.[11] Kulfan B M.Recent extensions and applications of the "CST" universal parametric geometry representation method.AIAA-2007-7709,2007.[12] Lane A K,Marshall D D.A surface parameterization method for airfoil optimization and high lift 2D geometries utilizing the CST methodology.AIAA-2009-1461,2009.[13] Jones R T.Theory of wing-body drag at supersonic speeds.NACA-RM-A53H18A,1953.[14] Chin W C.Supersonic wave-drag of planar singularity distributions.AIAA Journal,1978,16(5): 482-487.[15] Jumper E J.Wave drag prediction using a simplified supersonic area rule.Journal of Aircraft,1983,20(10): 893-895.[16] Bushgens G S.Aerodynamics,stability and controllability of supersonic aircraft.Guo Z,translated.Shanghai: Shanghai Jiaotong University Press,2009: 154-157.(in Chinese) Bushgens G S.超声速飞机空气动力学和飞行力学.郭桢,译.上海: 上海交通大学出版社,2009: 154-157. |
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